US2016238456A1PendingUtilityA1

Air temperature sensor and fabrication

Assignee: ROSEMOUNT AEROSPACE INCPriority: Feb 12, 2015Filed: Feb 12, 2015Published: Aug 18, 2016
Est. expiryFeb 12, 2035(~8.6 yrs left)· nominal 20-yr term from priority
Inventors:Scott Wigen
G01K 1/08G01K 1/14G01K 13/02G01K 13/028H05K 5/0213
35
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Claims

Abstract

A method is disclosed for making an air temperature sensor comprises first generating a digital model of an air temperature sensor housing. The digital model is inputted into an additive manufacturing apparatus comprising an energy source. The additive manufacturing apparatus applies energy from the energy source to successively applied incremental quantities of a fusible material. The energy source fuses the successively applied incremental quantities of the fusible material to form incremental portions of the air temperature sensor housing that accrete together to form the air temperature sensor housing

Claims

exact text as granted — not AI-modified
1 . A method for making an air temperature sensor, comprising
 generating a digital model of an air temperature sensor housing;   inputting the digital model into an additive manufacturing apparatus or system comprising an energy source and;   repeatedly applying energy from the energy source to successively applied incremental quantities of a fusible material to form the air temperature sensor housing corresponding to the digital model; and   disposing a temperature sensing element in the air temperature sensor housing.   
     
     
         2 . The method of  claim 1 , wherein the air temperature sensor housing includes an air inlet, a first conduit in fluid communication with the air inlet, an air outlet in fluid communication with the channel, and a sensor support structure configured to retain the temperature sensing element mounted in the channel. 
     
     
         3 . The method of  claim 2 , wherein the air temperature sensor housing includes at least one feature fabricated by said repeated application of energy to successively applied incremental quantities of fusible material, selected from:
 the sensor support structure, integral with the housing;   a non-circular opening in the first conduit as said outlet;   an air swirler integral with and extending inwardly from the first conduit;   an ice barrier integral with and extending inwardly from the first conduit; and   varied radial cross-section of the first conduit; and   varied surface texture on the inner surface of the first conduit.   
     
     
         4 . The method of  claim 3 , wherein the air temperature sensor housing includes the feature of the sensor support structure integral with the housing. 
     
     
         5 . The method of  claim 3 , wherein the air temperature sensor housing includes the feature of the non-circular opening in the first conduit as said outlet. 
     
     
         6 . The method of  claim 3 , wherein the air temperature sensor housing includes the feature of the air swirler integral with and extending inwardly from the first conduit. 
     
     
         7 . The method of  claim 3 , wherein the air temperature sensor housing includes the feature of the ice barrier integral with and extending inwardly from the first conduit. 
     
     
         8 . The method of  claim 3 , wherein the air temperature sensor housing includes the feature of varied surface texture on the inner surface of the first conduit. 
     
     
         9 . The method of  claim 2 , further comprising a second conduit disposed concentrically around the first conduit, thereby providing an annular air space between the first and second conduits that is in fluid communication with the inlet. 
     
     
         10 . The method of  claim 9 , wherein the air temperature sensor housing includes at least one feature fabricated by said repeated application of energy to successively applied incremental quantities of fusible material, selected from a support tab between the first and second conduits and non-circular openings in the second conduits as said outlet. 
     
     
         11 . The method of  claim 9 , wherein the first conduit has a radial cross-section that varies along the length of the first conduit. 
     
     
         12 . An air temperature sensor housing, comprising an air inlet, a first conduit in fluid communication with the air inlet, an air outlet in fluid communication with the channel, and a sensor support structure configured to retain a temperature sensor mounted in the channel, wherein the air temperature sensor housing includes at least one feature fabricated by said repeated application of energy to successively applied incremental quantities of fusible material, selected from:
 the sensor support structure, integral with the housing;   a non-circular opening in the first conduit as said outlet;   an air swirler integral with and extending inwardly from the first conduit;   an ice barrier integral with and extending inwardly from the first conduit; and   varied radial cross-section of the first conduit; and   varied surface texture on the inner surface of the first conduit.   
     
     
         13 . The housing of  claim 12 , further comprising a second conduit disposed concentrically around the first conduit, thereby providing an annular airflow space between the first and second conduits that is in fluid communication with the inlet. 
     
     
         14 . The housing of  claim 13 , wherein the air temperature sensor housing includes a support tab between the first and second conduits and non-circular openings in the second conduits as said outlet.

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